Quicksilver Aircraft

MX Sprint

Specifications:

POWERPLANT

PowerPlant	1 Rotax Model 447 Twin Cylinder, Two Cycle 436.5 cc, 40 hp @ 6500 rpm
Recommended TBO	300 hr
Propeller	66 in x 34 in
Length	18 ft 1 in
Height	8 ft 10 in
Wingspan	28 ft 0 in
Wing area	156 sq ft
Wing loading	3.36 lb/sq ft
Power loading	13.12 lb.hp
Seats	1
Minimum flight crew	1
Empty Weight	250 lbs
Useful load	275 lbs
Payload w/full fuel.	245 lbs
Max takeoff weight	525 lbs
Fuel capacity	5 U.S. gal

PERFORMANCE

Takeoff distance, ground roll	65 ft
Takeoff distance, 50 ft obstacle	200 ft
Rate of climb	900 ft/min
Max operating altitude	14,000 ft
Landing distance 50 ft obstacle (with brake)	200 ft
Landing distance ground roll (with brake)	60 ft

CRUISE PERFORMANCE CHART
(Speed/Range at sea level with 4.8 gal. usable fuel)

At 55% power(5300 rpm)	44 mph/84 mi
At 65% power(5600 rpm)	47 mph/84 mi
At 75% power(5900 rpm)	50 mph/80 mi
At 100% power(6500 rpm)	54 mph/52 mi

FUEL FLOW

At 55% power	2.5 gph
At 65% power	2.7 gph
At 75% power	3.0 gph
At 100% power	4.5 gph

LIMITING AND RECOMMENDED SPEEDS

Vx (Best angle of climb)	33 mph
Vy (Best rate of climb)	36 mph
Va (Design maneuvering)	48 mph
Vne (Never exceed).	65 mph
Vs (Stall, power off)	24 mph
Landing approach speed (1.3 Vs)	31 mph

KIT COST

Contact local dealer or Quicksilver for Price

Features

Rotax 447 Engine
Conventional 3-Axis Controls
66" Propeller for More Performance With Less Noise
Flexible Driveshaft Coupler for Reduced Vibration
Tapered Stabilizer
Tubular-Braced Tail
Triangulated Kingpost Assembly
Partial Double Surface Wings

Extra Ribs for Firm Airfoil
Excellent Crosswind Capability
Short Takeoff
Very Fast Control Response
Quicksilver's Famous Quality
Easy-to-Assemble Kit (Average 30 to 50) Hours)
6-Month Written Warranty (See Dealer for Details)

PRICES SUBJECT TO CHANGE WITHOUT NOTICE

All specifications are based on manufacturer's calculations.
All performance figures are based on standard day, standard atmosphere, at sea level and 175 lb. pilot weight,
unless otherwise noted.
Operations/equipment category reflects this aircraft's maximum potential.
The empty weight is approximate due to 6% Mil Spec tolerance on materials.
Only Quicksilver Manufacturing approved accessories should be installed on this aircraft.
This aircraft is not designed for aerobatics.
Be sure to follow the owners manual recommendations for flight and maintenance guidelines.
The pilot is responsible for operating this aircraft in accordance with the applicable Federal and State
Regulations
Range is listed in statute miles with no allowance for wind or fuel reserve.
*All performance figures are based on standard day, standard atmosphere, at sea level, and aircraft at 525
pounds take-off weight.
These distances must be increased equal to 20% for each one thousand feet of pressure altitude above sea level.
**The empty weight is approximate due to a 4% Mil. Spec. tolerance on materials.
Weight shown is minimum empty weight.

All specifications are based on manufacturers calculations.
SPECIFICATIONS SUBJECT TO CHANGE WITHOUT NOTICE.
This information is for reference only, please consult Quicksilver or
one of it’s dealers for exact and up to date specifications.